计算尖锥迎面干扰的一种新方法

本文从运动气流的二维激波动力学方程组出发,提出了一种计算平面运动激波和尖锥头激波迎面干扰问题的新方法。该方法可以计算穿透激波的强度和形状,马赫反射时三波点的轨迹,马赫杆的强度和几何形状,以及锥面峰值压力的大小。计算结果与数值模拟、其它计算方法以及实验数据进行了比较,结果表明本方法不仅精度较高,而且保持了简捷,省机时的优点。     

传输型光学遥感器斜模式采样新方法研究

文章介绍了实现超模式采样焦平面3种解决方案面临的技术难点,为避开器件问题提出了一 种新的斜模式采样方法。以任意两雏周期采样理论为基础分析了斜模式采样技术的物理原理,并通过实验 手段验证了斜模式采样技术的可行性。试验结果表明:改变探测器推扫方向的采样间距,斜模式采样技术 可以提高传输型光学遥感器图像的空间分辨率,该技术相对于超模式采样技术,工程实现上要简单。     

航空发动机小孔特种加工技术

航空发动机是技术密集、结构复杂的热力机械,是军用飞机和民用客机的主要动力.随着飞机各项性能的不断提高,对航空发动机也提出了更高的要求,各种新结构、新材料和复杂形状的精密零部件大量应用于航空发动机中,显著增加了航空发动机的制造难度.     

基于导航定位原理的火箭涡轮泵轴承故障诊断

为准确判断火箭发动机涡轮泵轴承在试验台上试验时发生故障的部位，同时避免通过轴承特征频率诊断轴承故障的方法所带来的不确定性，基于GPS卫星导航定位原理，利用时幅曲线的相位信息，提出一种新的轴承故障诊断方法:振源坐标定位法，即通过四个已知坐标的振动传感器测得同一振动波的时幅曲线相位差判定振源位置。将试验台上轴承和四个振动信号传感器安放在坐标已知的直角坐标系中，利用时幅曲线拐点分析法准确捕获振动信号到达四个传感器的时刻，再利用这四个时刻和已知坐标计算出振源位置坐标，最后根据振源位置坐标判断其是否为轴承故障及具体故障部位。通过仿真计算证明该方法理论上可行。     

冷阴极电离真空计校准方法研究

主要介绍了冷阴极电离真空计结构、工作原理及冷阴极电离真空计的校准方法和校准装置,并对校准数据进行了处理。由于冷阴极电离真空计为非线性真空计,通过比较,校准结果采用了校准曲线的方式,可提高校准的准确度,减小校准不确定度,保证真空测量的可靠性。     

Fault-tolerant control with mixed aerodynamic surfaces and RCS jets for hypersonic reentry vehicles

This paper proposes a fault-tolerant strategy for hypersonic reentry vehicles with mixed aerodynamic surfaces and reaction control systems (RCS) under external disturbances and subject to actuator faults. Aerodynamic surfaces are treated as the primary actuator in normal situations, and they are driven by a continuous quadratic programming (QP) allocator to generate torque com-manded by a nonlinear adaptive feedback control law. When aerodynamic surfaces encounter faults, they may not be able to provide sufficient torque as commanded, and RCS jets are activated to augment the aerodynamic surfaces to compensate for insufficient torque. Partial loss of effective-ness and stuck faults are considered in this paper, and observers are designed to detect and identify the faults. Based on the fault identification results, an RCS control allocator using integer linear programming (ILP) techniques is designed to determine the optimal combination of activated RCS jets. By treating the RCS control allocator as a quantization element, closed-loop stability with both continuous and quantized inputs is analyzed. Simulation results verify the effectiveness of the proposed method.     

英语诗歌教学探析

面对已经被"边缘化"的英语诗歌教学,从提高人文素养的角度出发,分析当前高等教育英语专业中英语诗歌教学的不利因素,并总结几种教学方法使学生可以更好的欣赏英语诗歌,也可以更进一步提高自我的人文素养。     

柴油机螺旋进气道结构参数对气道性能的影响分析

对柴油机螺旋气道结构参数进行了流动特性敏感分析。采用数值模拟与测试结合的方法,对柴油机进气道最小截面的不同修改方案的流动特性进行了研究,分析了不同升程下气道性能影响因素与变化趋势。研究表明:小气门升程时,气道性能由气门开启面积决定;中大气门升程时,气道最小截面积是影响气道性能的主要结构参数之一,在螺旋进气道修正设计过程中应予以充分重视。与原气道对比,适当增加气道螺旋段外侧面积,可以提高平均涡流比;适当增加气道螺旋段内侧面积,可以提高平均流量系数。     

基于MiniGUI的嵌入式显控系统的设计与实现

MiniGUI是目前比较成熟图形用户接口,具有小巧、可配置和可移植等特点,本文结合触摸显控处理机实际项目开发和应用,重点研究了基于MiniGUI的嵌入式Linux图形系统的开发.     

Coastal sea level changes in Europe from GPS,tide gauge,satellite altimetry and GRACE, 1993–2011

Sea level changes are threatening the human living environments, particularly along the European Coasts with highly dense population. In this paper, coastal sea level changes in western and southern Europe are investigated for the period 1993–2011 using Global Positioning System (GPS), Tide Gauge (TG), Satellite Altimetry (SA), Gravity Recovery and Climate Experiment (GRACE) and geophysical models. The mean secular trend is 2.26 ± 0.52 mm/y from satellite altimetry, 2.43 ± 0.61 mm/y from TG+GPS and 1.99 ± 0.67 mm/y from GRACE mass plus steric components, which have a remarkably good agreement. For the seasonal variations, annual amplitudes of satellite altimetry and TG+GPS results are almost similar, while GRACE Mass+Steric results are a little smaller. The annual phases agree remarkably well for three independent techniques. The annual cycle is mainly driven by the steric contributions, while the annual phases of non-steric (mass component) sea level changes are almost a half year later than the steric sea level changes.